Textron Inc.
Adaptive engine exhaust signature suppressor

Last updated:

Abstract:

An exhaust system has an engine exhaust plane associated with an entrance to the exhaust system, an exhaust exit plane associated with an exit of the exhaust system, a forward cap movable relative to the engine exhaust plane and configured to selectively intersect the engine exhaust plane, and an aft cap movable relative to the exhaust exit plane and configured to selectively intersect the exhaust exit plane.

Status:
Grant
Type:

Utility

Filling date:

4 Apr 2016

Issue date:

29 Oct 2019